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gptkbp:instanceOf
|
gptkb:surface-to-air_missile
|
|
gptkbp:deployment
|
hardened shelters
open launchers
|
|
gptkbp:engineType
|
ramjet
solid-fuel rocket booster
|
|
gptkbp:firstFlight
|
1952
|
|
gptkbp:fullName
|
gptkb:Boeing_CIM-10_BOMARC
|
|
gptkbp:guidanceSystem
|
semi-active radar homing
command guidance
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
BOMARC
|
|
gptkbp:introduced
|
1959
|
|
gptkbp:length
|
14 m
|
|
gptkbp:manufacturer
|
gptkb:Boeing
gptkb:Michigan_Aerospace_Research_Center
|
|
gptkbp:notableEvent
|
involved in the 1960 BOMARC missile accident in New Jersey
deployed during the Cold War
first long-range anti-aircraft missile deployed by the US
|
|
gptkbp:numberBuilt
|
about 700
|
|
gptkbp:predecessor
|
none
|
|
gptkbp:primaryUse
|
long-range air defense
|
|
gptkbp:range
|
400 km
|
|
gptkbp:retired
|
1972
|
|
gptkbp:speed
|
Mach 2.8
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Nike_Hercules
|
|
gptkbp:usedBy
|
gptkb:United_States_Air_Force
gptkb:Royal_Canadian_Air_Force
|
|
gptkbp:warheadType
|
gptkb:W40_nuclear_warhead
conventional high-explosive warhead
|
|
gptkbp:weight
|
7,000 kg
|
|
gptkbp:wingspan
|
5.5 m
|
|
gptkbp:bfsParent
|
gptkb:Air_Defense_Command
|
|
gptkbp:bfsLayer
|
6
|